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Sketch the ground track (3 orbital periods) of a satellite on an elliptical orbit with inclination of 50, argument of perigee 270, and 4 hour

Sketch the ground track (3 orbital periods) of a satellite on an elliptical orbit with inclination of 50, argument of perigee 270, and 4 hour orbital period. You may assume that at time t = 0, the spacecraft was ascending above the equator at 90 of eastern longitude. Map is provided

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